Artículo de Publicación Periódica:
Hardware in the loop and software in the loop testing of the MOVE-II CubeSat

dc.contributor.authorKiesbye, Jonis
dc.contributor.authorMessmann, David
dc.contributor.authorPreisinger, Maximiliam
dc.contributor.authorReina Kiperman, Gonzalo Julián
dc.contributor.authorNagy, Daniel
dc.contributor.authorSchummer, Florian
dc.contributor.authorMostad, Martin
dc.contributor.authorKale, Tejas
dc.contributor.authorLanger, Martin
dc.date.accessioned2020-03-26T14:44:26Z
dc.date.available2020-03-26T14:44:26Z
dc.date.issued2019-12
dc.description.abstract"This article reports the ongoing work on an environment for hardware-in-the-loop (HIL) and software-in-the-loop (SIL) tests of CubeSats and the benefits gained from using such an environment for low-cost satellite development. The satellite tested for these reported efforts was the MOVE-II CubeSat, developed at the Technical University of Munich since April 2015. The HIL environment has supported the development and verification of MOVE-II’s flight software and continues to aid the MOVE-II mission after its launch on 3 December 2018. The HIL environment allows the satellite to interact with a simulated space environment in real-time during on-ground tests. Simulated models are used to replace the satellite’s sensors and actuators, providing the interaction between the satellite and the HIL simulation. This approach allows for high hardware coverage and requires relatively low development effort and equipment cost compared to other simulation approaches. One key distinction from other simulation environments is the inclusion of the electrical domain of the satellite, which enables accurate power budget verification. The presented results include the verification of MOVE-II’s attitude determination and control algorithms, the verification of the power budget, and the training of the operator team with realistic simulated failures prior to launch. This report additionally presents how the simulation environment was used to analyze issues detected after launch and to verify the performance of new software developed to address the in-flight anomalies prior to software deployment."en
dc.identifier.issn2226-4310
dc.identifier.urihttp://ri.itba.edu.ar/handle/123456789/1917
dc.language.isoenen
dc.relationinfo:eu-repo/semantics/altIdentifier/doi/10.3390/aerospace6120130
dc.relationinfo:eu-repo/grantAgreement/BMWi/DLR/50RM1509/GR. Berlín
dc.rightshttps://creativecommons.org/licenses/by/4.0/
dc.subjectHARDWAREen
dc.subjectSOFTWAREen
dc.subjectSIMULACIONes
dc.subjectSATELITESes
dc.titleHardware in the loop and software in the loop testing of the MOVE-II CubeSaten
dc.typeArtículos de Publicaciones Periódicases
dc.typeinfo:eu-repo/semantics/publishedVersion
dspace.entity.typeArtículo de Publicación Periódica
itba.description.filiationFil: Kiesbye, Jonis. Technische Universität München; Alemania
itba.description.filiationFil: Messmann, David. Technische Universität München; Alemania.
itba.description.filiationFil: Preisinger, Maximiliam. Technische Universität München; Alemania.
itba.description.filiationFil: Reina Kiperman, Gonzalo Julián. Instituto Tecnológico de Buenos Aires; Argentina.
itba.description.filiationFil: Nagy, Daniel. Technische Universität München; Alemania.
itba.description.filiationFil: Schummer, Florian. Technische Universität München; Alemania.
itba.description.filiationFil: Mostad, Martin. Norges Teknisk-Naturvitenskapelige Universitet; Noruega.
itba.description.filiationFil: Kale, Tejas. Technische Universität München; Alemania.
itba.description.filiationFil: Langer, Martin. Technische Universität München; Alemania.
itba.description.filiationFil: Langer, Martin. Orbital Oracle Technologies GmbH; Alemania
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